Integrated PID controller design for an unmanned aerial vehicle with static stability
This paper presents an integrated guidance and control (IGC) design method for an unmanned aerial vehicle with static stability which is described by a nonlinear six-degree-of-freedom (6-DOF) model. The model is linearized by using small disturbance linearization. The dynamic characteristics of pitc...
| Main Authors: | , , |
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| Format: | Journal Article |
| Published: |
Cambridge University Press
2013
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| Online Access: | http://hdl.handle.net/20.500.11937/52221 |